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just like the -230 and -231/-231EX were slightly modified to strengthen the fuselage structure after a fatal accident in 2005 which grounded them for a full year. Fuselage rib n°2 holding the landing gear and the wing spar has been reinforced externally and internally. The planes are now back to
286:
wing was specially designed for durability and light weight. The design has won the World
Championships in 1998, 2000 and 2007, as well as a number of other national-level competitions. It has a roll rate of 420° per second and a climb rate of nearly 3,300 feet per minute.
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was developed in 1990. The fuselage design remained unchanged and only leading edge triangular apex surfaces were added to reduce buffeting during high G pullups. The CAP 231 was world champion in 1990. Between 1990-1998 this was the mount of the
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competition single seater strengthened to cope with a 300 hp (220 kW) 6-cylinder
Lycoming AEIO-540 engine instead of the 200 hp (150 kW) original 4-cylinder Lycoming AEIO-360.
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competition and came second (individual with a -231EX), sixth with a -232, and first team at the WAC 2007. In the years 1999-2005, examples were flown by the French Air Force aerobatics team.
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and a full wooden construction. It withstood +10/-10 G-forces, had a 270 degrees/second roll rate and a top speed of 400 km/h. Between 1986-1990 this was the mount of the
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was primarily developed in 1985 for the French Air Force. From the basic CAP 21 airframe, trailing edge apex triangular surfaces were added to the basic
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wing taken from an EXTRA 260 (thus the -EX name) was adapted to a few CAP 231 airframes.
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6-cylinder air-cooled horizontally-opposed piston engine, 224 kW (300 hp)
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658:(84th ed.). Coulson, Surrey, UK: Jane's Information Group. pp. 87–88.
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Mike
Gallaway's Mudry CAP 230 at the 2019 Fort Worth Alliance Air Show
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Aircraft produced by Centre-Est Aéronautique - Avions Pierre Robin -
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Taylor, Michael J.H.; Lambert, mARK; Munson, Kenneth, eds. (1993).
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evolved in 1994. While the fuselage construction retained wood, a
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228:. The CAP 230 airframe was a direct development of the
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65 L (17 US gal; 14 imp gal)
597:"Equipe de Voltige de l'Armée de l'Air - historique"
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Aircraft of comparable role, configuration, and era
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270°/s at 300 km/h (190 mph; 160 kn)
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46:. Unsourced material may be challenged and removed.
366:Airclubs and privates own planes of all subtypes.
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8:
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727:
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117:
500:400 km/h (250 mph, 220 kn)
485:300 km/h (190 mph, 160 kn)
479:330 km/h (210 mph, 180 kn)
349:aerobatic team owned CAP 230, 231 and 232
106:Learn how and when to remove this message
656:Jane's all the world's aircraft, 1993-94
681:"The Incomplete Guide to Airfoil Usage"
581:
506:360 km (220 mi, 190 nmi)
377:Jane's All The World's Aircraft 1993–94
491:90 km/h (56 mph, 49 kn)
464:3 or 4-bladed constant-speed propeller
601:Equipe de Voltige de l'Armée de l'Air
254:Equipe de Voltige de l'Armée de l'Air
7:
591:
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533:74 kg/m (15 lb/sq ft)
271:To increase performance, in 1991, a
44:adding citations to reliable sources
415:9.86 m (106.1 sq ft)
403:8.08 m (26 ft 6 in)
397:6.75 m (22 ft 2 in)
14:
542:0.31 kW/kg (0.19 hp/lb)
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409:1.9 m (6 ft 3 in)
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20:
857:Single-engined tractor aircraft
527:16 m/s (3,100 ft/min)
31:needs additional citations for
150:Competition aerobatic aircraft
1:
872:Aircraft first flown in 1997
160:Avions Mudry & Cie (now
847:1990s French sport aircraft
442:820 kg (1,808 lb)
436:730 kg (1,609 lb)
430:630 kg (1,389 lb)
893:
877:Conventional landing gear
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322:8 aircraft, flown by the
252:aerobatics team (French:
224:designed for competition
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456:Lycoming AEIO-540-L1 B5D
370:Specifications (CAP 231)
324:Royal Moroccan Air Force
685:m-selig.ae.illinois.edu
382:General characteristics
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236:Design and development
220:family is a family of
716:at Wikimedia Commons
361:
40:improve this article
623:"German-Aerobatics"
440:Max takeoff weight:
142:General information
867:Aerobatic aircraft
496:Never exceed speed
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173:Moroccan Air Force
852:Low-wing aircraft
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712:Media related to
679:Lednicer, David.
326:air display team
268:aerobatics team.
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184:Introduction date
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55:"Mudry CAP 230"
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703:External links
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665:978-0710610669
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629:on 2012-05-02.
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525:Rate of climb:
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96:December 2009
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57: –
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51:Find sources:
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29:This article
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18:
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688:. Retrieved
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627:the original
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607:30 September
605:. Retrieved
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563:Sukhoi Su-26
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328:Marche Verte
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284:carbon-fiber
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273:carbon-fiber
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215:CAP Aviation
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206:Mudry CAP-20
192:First flight
169:Primary user
156:Manufacturer
102:
93:
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62:
50:
38:Please help
33:verification
30:
470:Performance
462:Propellers:
452:Powerplant:
424:V16F (16%)
132:CAP-232 at
841:Categories
771:CAP 10C NG
576:References
538:Power/mass
519:Roll rate:
413:Wing area:
226:aerobatics
66:newspapers
641:"Results"
568:Extra 300
510:g limits:
401:Wingspan:
375:Data from
299:Operators
280:CAP 231EX
690:16 April
547:See also
354:Civilian
304:Military
222:aircraft
420:Airfoil
407:Height:
395:Length:
318:Morocco
292:CAP 232
261:CAP 231
242:CAP 230
218:CAP-23x
179:History
134:Airexpo
121:CAP 232
80:scholar
806:HR.200
801:HR.100
796:DR.500
791:DR.400
786:DR.300
781:DR.200
776:DR.100
662:
504:Range:
341:France
338:
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230:CAP 21
82:
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53:
821:R3000
816:R2000
811:R1000
389:Crew:
87:JSTOR
73:books
692:2019
660:ISBN
609:2018
454:1 ×
345:The
290:The
278:The
259:The
240:The
213:The
196:1997
187:1998
147:Type
136:2007
59:news
766:ATL
256:).
42:by
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826:X4
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599:.
584:^
515:10
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513:±
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391:1
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103:(
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84:·
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70:·
63:·
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